Sigma 5: Difference between revisions
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The ©rusader (talk | contribs) (Created page with "{{Infobox spaceflight | name = Sigma-5 | image = MascCosmonaut 1.png | image_caption = Cosmounaut rank 1 TBA photographed by cosmonaut...") |
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| mission_type = Crewed lunar landing | | mission_type = Crewed lunar landing | ||
| operator = [[ | | operator = [[File:Maoa.png|25px]][[MAOA]]<br>[[File:DulebianSpaceAgency.png|25px]][[People's Republic of Dulebia space program]] | ||
| COSPAR_ID = Hmm | | COSPAR_ID = Hmm | ||
| SATCAT = Hmm | | SATCAT = Hmm | ||
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| programme = [[Sigma program]] | | programme = [[Sigma program]] | ||
}} | }} | ||
==Background== | |||
==Crew and mission control== | |||
===Mascyllary crew=== | |||
===Dulebian crew=== | |||
==Planning and training== | |||
===Incidents=== | |||
==Hardware== | |||
===Spacecraft=== | |||
===Launch vehicle=== | |||
===Space suits=== | |||
===Lunar rover-?=== | |||
==Mission summary== | |||
===Launch and outbound trip=== | |||
===Landing=== | |||
===Lunar surface=== | |||
===Return to Earth=== | |||
==Legacy== | |||
==Commemorations== | |||
==Gallery-?== | |||
==See also== | |||
*[[MAOA]] | |||
*[[People's Republic of Dulebia space program]] | |||
Revision as of 00:20, 14 April 2020
 Cosmounaut rank 1 TBA photographed by cosmonaut rank 2 TBA | |
| Mission type | Crewed lunar landing |
|---|---|
| Operator |  MAOA People's Republic of Dulebia space program |
| COSPAR ID | Hmm |
| SATCAT no. | Hmm |
| Mission duration | 11 days, 1 hour, 51 minutes, 5 seconds (from Apollo 15) |
| Spacecraft properties | |
| Spacecraft |
|
| Manufacturer |
|
| Launch mass | 107,226 pounds (48,637 kg) |
| Landing mass | 11,995 pounds (5,441 kg) |
| Crew | |
| Crew size | 3 |
| Members |
|
| Callsign |
|
| EVAs | 1 in cislunar space to retrieve film cassettes - ? |
| EVA duration | 1 h 23 min 42 s - ? |
| Start of mission | |
| Launch date | 1979, 00:00:00 UTC |
| Rocket | Atlant-3 |
| Launch site | TBD |
| End of mission | |
| Recovered by | CRS Wagemut |
| Landing date | 1979, 19:45:05 UTC |
| Landing site | TBD |
| Orbital parameters | |
| Reference system | Selenocentric |
| Periselene altitude | 20.2 kilometers (10.9 nmi) - ? |
| Aposelene altitude | 108.3 kilometers (58.5 nmi) - ? |
| Epoch | 1979, 00:00 UTC |
| Template:Infobox spaceflight/Dock Template:Infobox spaceflight/Dock | |
| Payload | |
| Mass |
|
 Left to right: TBA, TBA, TBA | |